# N642CA: 2026 Cirrus Design SR22T

- Status: Valid registration
- Airframe: [Cirrus Design SR22T](https://openairdocs.org/model/cirrus-design-sr22t) (registry code 2130004, 5 seats)
- Engine: [Continental TSIO-550-K](https://openairdocs.org/engine/continental-tsio-550-k) (registry code 17410)
- Data sheets: [TCDS A00009CH](https://openairdocs.org/tcds/A00009CH) (Cirrus Design Corporation), [TCDS E5SO](https://openairdocs.org/tcds/E5SO) (Continental Aerospace Technologies, Inc.) (OpenAirDocs)
- Serial number: 11479
- Year built: 2026
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: June 26, 2026
- Certificate issued: October 10, 2026
- Expires: October 31, 2033
- Mode S code: A86CDC
- Registered owner: [110 Aviation LLC](https://openairdocs.org/faa-owner/110%20AVIATION%20LLC)
- Location: [West Des Moines, IA](https://openairdocs.org/faa-place/IA/West%20Des%20Moines)
- Owner type: LLC
- Owner's area on the map: 41.5624° N, 93.8117° W: Placed by OpenAirDocs at the center of ZIP code 50266, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=642CA
- Page: https://openairdocs.org/aircraft/N642CA

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 17 in force

### Matched by airframe (Cirrus Design SR22T)

- [AD 2024-24-11](https://openairdocs.org/ad/2024-24-11): Power Lever · Cirrus Design SR20, SR22 and SR22T. Effective Dec 23, 2024
- [AD 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023
- [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2012-01-11](https://openairdocs.org/ad/2012-01-11): Engine Air Intake · Cirrus Design SR22T. Effective Feb 29, 2012

### Matched by engine (Continental TSIO-550-K)

- [AD 2023-05-16](https://openairdocs.org/ad/2023-05-16): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 147 more. Effective Mar 15, 2023
- [AD 2023-02-12](https://openairdocs.org/ad/2023-02-12): Engine Air Intake System · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 127 more. Effective Feb 17, 2023
- [AD 2020-16-11](https://openairdocs.org/ad/2020-16-11): SUMMARY: Reciprocating Cylinder Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 23 more. Effective Sep 21, 2020
- [AD 2016-21-04](https://openairdocs.org/ad/2016-21-04): Oil cooler cross fitting assembly · Continental Motors TSIO-550-C, TSIO-550-K, TSIO-550-N and 2 more. Effective Nov 18, 2016
- [AD 2016-16-12](https://openairdocs.org/ad/2016-16-12): Cylinder assemblies · Continental Motors LTSIO-520-AE, TSIO-520-A, TSIO-520-AE and 89 more. Effective Sep 15, 2016
- [AD 2012-10-13](https://openairdocs.org/ad/2012-10-13): Starter adapters · Continental Motors IO-550-N, TSIO-520-B, TSIO-520-BB and 14 more. Effective Jun 8, 2012
- [AD 2012-03-06](https://openairdocs.org/ad/2012-03-06): Fuel servo diaphragm · Continental Motors 6-260-A, 6-285-A, 6-285-B and 482 more. Effective Feb 24, 2012
- [AD 2010-11-04](https://openairdocs.org/ad/2010-11-04): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 190 more. Effective Jun 16, 2010
- [AD 2004-08-10](https://openairdocs.org/ad/2004-08-10): Serial-numbered (SN) cylinders · Modify Teledyne Continental TSIO-520-NB engine (RAM Aircraft Limited Partnership STC SE09104SC or 4 others). Effective May 5, 2004
- [AD 2000-23-21](https://openairdocs.org/ad/2000-23-21): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 164 more. Effective Dec 12, 2000
- [AD 99-19-01](https://openairdocs.org/ad/99-19-01): No. 2 and No. 5 Crankshaft Inspections · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 127 more. Effective Sep 30, 1999
- [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996
- [AD 93-10-02](https://openairdocs.org/ad/93-10-02): Missing Cylinder Valve Retainer Key · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 180 more. Effective Aug 12, 1993

### Historical (superseded or no longer in force)

- [AD 2023-04-08](https://openairdocs.org/ad/2023-04-08) (historical): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 141 more. Effective Feb 23, 2023
- [AD 2011-25-51](https://openairdocs.org/ad/2011-25-51) (historical): Starter Adapter Gear Shaft · Continental Motors IO-550-N, TSIO-520-B, TSIO-520-BB and 14 more. Effective Dec 28, 2011
- [AD 2009-24-52](https://openairdocs.org/ad/2009-24-52) (historical): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 192 more

## Information bulletins (advisory) (8 in force)

- [SAIB CE-13-43R1](https://openairdocs.org/saib/CE-13-43R1): Aircraft Fuel Distribution System and Ice/Rain Protection System. Issued Sep 30, 2013
- [SAIB CE-11-50](https://openairdocs.org/saib/CE-11-50): Flight Controls, Flaps. Issued Aug 26, 2011
- [SAIB NE-20-05](https://openairdocs.org/saib/NE-20-05): POWERPLANT - Engine Camshaft Gear Tooth Fracture. Issued Apr 6, 2020
- [SAIB NE-18-16](https://openairdocs.org/saib/NE-18-16): POWERPLANT  Alternator Drive Coupling. Issued Jun 20, 2018
- [SAIB NE-17-11](https://openairdocs.org/saib/NE-17-11): POWERPLANT  Engine damage as a result of kickback. Issued May 10, 2017
- [SAIB NE-16-13](https://openairdocs.org/saib/NE-16-13): Powerplant - Prohibited use of sealant. Issued Mar 8, 2016
- [SAIB NE-13-15](https://openairdocs.org/saib/NE-13-15): Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control Levers. Issued Feb 8, 2013
- [SAIB NE-13-04](https://openairdocs.org/saib/NE-13-04): Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing Inspection. Issued Oct 31, 2012
- [SAIB CE-13-43](https://openairdocs.org/saib/CE-13-43) (historical): Aircraft Fuel Distribution System and Ice/Rain Protection System. Issued Aug 30, 2013

## NTSB investigations

None matched to N642CA.

## FAA accident and incident reports

None matched to N642CA.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N642CA not matched to an aircraft (121, newest 50)

They name N642CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR N6WA201906030001](https://openairdocs.org/sdr/N6WA201906030001), May 30, 2019: STAY. DAMAGED. RIGHT MAIN LANDING GEAR DISAGREE DURING EXTENSION FOR LANDING. WORK ACCOMPLISHED ON NRWO 23401-1. R & R RH MLG SIDE STAY ASSY IAW AMM 32-11-12. OPS CHECK GOOD A
- [SDR N6WA2019052402](https://openairdocs.org/sdr/N6WA2019052402), May 24, 2019: BATTERY. DISCHARGED. CA SIDE EMERGENCY FLASHLIGHT NOT BLINKING. R&R CAPTAIN SIDE EMERGENCY FLASHLIGHT BATTERY IAW CMM 25-60-02. OPS CHECK GOOD. OK FOR SERVICE.
- [SDR N6WA2019052301](https://openairdocs.org/sdr/N6WA2019052301), May 23, 2019: LIGHT. INOPERATIVE. OVERHEAD EMERGENCY LIGHT AT ROW 18 IS INOP. AS PER TELECOM MXC, DEFERRED OVERHEAD EMERGENCY LIGHT AT ROW 18 ON OCN 70056134 PER MEL33-51-01B CAT C.
- [SDR V0XD20180306548](https://openairdocs.org/sdr/V0XD20180306548), Mar 6, 2018: RETAINER. BENT. PASSENGER DOOR SEAL RETAINER BENT ON BOTTOM FORWARD SIDE. REMOVED AND REPLACED THE SEAL RETAINER IAW SRM 51-42-06, 51-40-11, 51-25-16, 51-42-13, AND AMM 52-11-0
- [SDR V0XD20180301003](https://openairdocs.org/sdr/V0XD20180301003), Mar 1, 2018: BRACKET. CRACKED. PASSENGER DOOR INTERNAL STRUCTURE UPPER AFT L BRACKET IS CRACKED. REMOVED AND REPLACED THE BRACKET IAW SRM 51-40-11, 51-42-06, 51-42-21, 51-42-13 AND 51-42-22.
- [SDR V0XD2018022210125](https://openairdocs.org/sdr/V0XD2018022210125), Feb 21, 2018: FORMER. CORRODED. PASSENGER FORMER AT FS 311.75 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED PASSENGER DOOR FORMER AT FS 311.75 IAW SRM 51-42-06, 51-40-11, 51-25-16, 51-42-10,
- [SDR V0XD20180306007](https://openairdocs.org/sdr/V0XD20180306007), Feb 17, 2018: DRAG ANGLE. CRACKED. PASSENGER DOOR AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW SRM 51-42-06, 51-40-11, 51-25-16, 51-25-06, 51-21-11, AND 52
- [SDR V0XD20180303DP01](https://openairdocs.org/sdr/V0XD20180303DP01), Feb 2, 2018: SKIN. CORRODED. PAX DOOR INTERIOR SKIN CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE SKIN ON THE PAX DOOR IAW SRM 51-42-06, AND SRM 51-42-10.
- [SDR V0XD20170217DP01](https://openairdocs.org/sdr/V0XD20170217DP01), Feb 1, 2018: WEB. CRACKED. AFT PAX DOOR WEB AT LOWER WHEEL SUPPORT HAS A CRACK. REPAIRED THE AFT PAX DOOR WEB IAW REO 670-52-11-999.
- [SDR V0XD20180117004](https://openairdocs.org/sdr/V0XD20180117004), Jan 17, 2018: FRAME. CORRODED. FRAME BS 310 CORRODED OUT OF LIMITS AT STRINGER 27. REMOVED AND REPLACED THE SECTION OF THE FRAME IAW REO 670-53-21-799, REV A, AND REO 670-53-21-1486, REV --.
- [SDR V0XD20180117003](https://openairdocs.org/sdr/V0XD20180117003), Jan 17, 2018: STRINGER. CORRODED. FUSELAGE STRINGER 26R CORRODED OUT OF LIMITS BETWEEN FS 295 AND 310. REMOVED AND REPLACED DAMAGED SECTION OF STRINGER 26R IAW SRM 53-00-03, 51-40-11, 51-42-06, 
- [SDR V0XD20180117002](https://openairdocs.org/sdr/V0XD20180117002), Jan 17, 2018: STRINGER. CORRODED. FUSELAGE STRINGER 25R CORRODED OUT OF LIMITS BETWEEN FS 280 AND 295. REMOVED AND REPLACED DAMAGED SECTION OF STRINGER 25R IAW SRM 53-00-03, 51-25-06, 51-40-11, 
- [SDR V0XD20180117001](https://openairdocs.org/sdr/V0XD20180117001), Jan 17, 2018: FRAME. CORRODED. FRAME 364 CORRODED OUT OF LIMITS BETWEEN STRINGERS 26L AND 25R. REMOVED AND REPLACED DAMAGED FRAME 364 SECTION BETWEEN STRINGERS 25L AND 25R IAW REO 670-53-21-6
- [SDR V0XD20180116002](https://openairdocs.org/sdr/V0XD20180116002), Jan 16, 2018: DRAG ANGLE. CRACKED. AFT DRAG ANGLE ON THE LH SIDE OF THE VERTICAL STABILIZER IS CRACKED. CORRECTIVE ACTION: REPAIRED AFT DRAG ANGLE ON THE LH SIDE OF THE VERTICAL STABLIZER IAW BOM
- [SDR V0XD20180116001](https://openairdocs.org/sdr/V0XD20180116001), Jan 16, 2018: HOUSING. CRACKED. AFT CARGO DOOR HANDLE HOUSING IS CRACKED IN TWO SPOTS. REMOVED AND REPLACED THE AFT CARGO DOOR HANDLE HOUSING IAW SRM 51-40-11, 51-42-21, 51-25-16, 51-42-06, 51
- [SDR V0XD20180116004](https://openairdocs.org/sdr/V0XD20180116004), Jan 16, 2018: STRINGER. DAMAGED. STRINGER 19L BETWEEN FS 1000 AND FS 1015 IS DAMAGED. REMOVED DAMAGED AREA OF STRINGER 19L AND SPLICED IN NEW SECTION IAW SRM 51-42-06, 51-42-21, 53-00-03, 51-25
- [SDR V0XD20180115003](https://openairdocs.org/sdr/V0XD20180115003), Jan 15, 2018: CAP. CORRODED. PASSNEGER DOOR MID CAP IS CORRODED. REMOVED AND REPLACED THE CAP IAW SRM 51-42-02, 51-42-10, 51-21-23, 51-40-11, 51-42-13, AND AMM 52-70-04,
- [SDR V0XD2017011201](https://openairdocs.org/sdr/V0XD2017011201), Jan 12, 2018: SKIN. GOUGED. AFT CARGO DOOR HAS A GOUGE ON THE TOP CENTER OUTER EDGE. CORRECTIVE ACTION: REPAIRED IAW REO 670-52-31-088 REV.-, SRM 51-25-16, 51-25-06, 51-21-11, 51-21-00, 51
- [SDR V0XD20180111002](https://openairdocs.org/sdr/V0XD20180111002), Jan 11, 2018: INTERCOSTAL. CORRODED. INTERCOSTAL BELOW GALLEY SERVICE DOOR BETWEEN BS 319.70 AND 349 HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21.
- [SDR V0XD20180111001](https://openairdocs.org/sdr/V0XD20180111001), Jan 11, 2018: INTERCOSTAL. CORRODED. INTERCOSTAL BELOW GALLEY SERVICE DOOR BETWEEN BS 310 AND 319.70 HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21.
- [SDR V0XD2018011100004](https://openairdocs.org/sdr/V0XD2018011100004), Jan 9, 2018: RIB. CRACKED. RIGHT HAND FIXED LEADING EDGE OUTBOARD RIB IS CRACKED. REMOVED AND REPLACED R/H FIXED LEADING EDGE O/B RIB(PN:CC670-12137-6) IAW SRM 51-42-06, 51-42-10, AND 51-
- [SDR V0XD20180109002](https://openairdocs.org/sdr/V0XD20180109002), Jan 9, 2018: WEB. CRACKED. FWD EQUIPMENT BAY LT FLOOR WEB AT BS 192 CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR IAW REO 670-53-11-509, REV D, SRM 51-21-11, 51-25-06, 51-25-
- [SDR V0XD20180109001](https://openairdocs.org/sdr/V0XD20180109001), Jan 9, 2018: SEAT TRACK. CORRODED. LT FLOOR SEAT RAIL AT FS 581-677 HAS SIGNS OF CORROSION. EVALUATED AND FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013 REV J DATED 2014/10/22. REMOVED AND REPLA
- [SDR V0XD20180110003](https://openairdocs.org/sdr/V0XD20180110003), Jan 8, 2018: CROSSBEAM. CRACKED. FS 280.00 CROSSBEAM LT AND RT SIDES ARE CRACKED. REMOVED AND REPLACED FS 280.00 CROSSBEAM (PN:CC670-34175-7S) IAW SRM 51-42-13, 51-42-21, 51-42-06, 51-11-41, 51
- [SDR V0XD20180116003](https://openairdocs.org/sdr/V0XD20180116003), Dec 24, 2017: PLATE. DAMAGED. DAMAGE TO AFT CARGO STRIKE PLATE BETWEEN FS1000-1047. COMPLETED REPAIR OF DAMAGE BELOW AFT CARGO STRIKE PLATE BETWEEN FS1000-1047 IAW REO 670-53-61-1428 DATED 2
- [SDR N6WA2017022501](https://openairdocs.org/sdr/N6WA2017022501), Feb 25, 2017: WARNING LIGHT. FALSE ACTIVATION. RIGHT EMERGENCY EXIT AMBER INDICATION. PERFORMED INSPECTION AND OPS CHECK IAW AMM 52-21-00. NO DEFECTS NOTED AT THIS TIME.
- [SDR N6WA2016061803](https://openairdocs.org/sdr/N6WA2016061803), Jun 18, 2016: DOOR. NOT CLOSED. CABIN FAILED TO PRESSURIZE. PERFORMED GENERAL VISUAL INSPECTION AND FOUND AFT CARGO DOOR NOT COMPLETELY CLOSED. GAP WAS FOUND TO BE ENOUGH TO NOT PRESSURIZE. PE
- [SDR N6WA2016052002](https://openairdocs.org/sdr/N6WA2016052002), May 20, 2016: PROXIMITY SWITCH. DIRTY. PASSENGER DOOR LATCH CAUTION MSG DISPLAYED WITH MEL 52-70-01 & 21-24-07. CLEANED PROXIMITY SWITCH AS REQUIRED. PERFORMED OPERATIONS CHECK OF THE PAX DOOR WARNIN
- [SDR N6WA2015090101](https://openairdocs.org/sdr/N6WA2015090101), Sep 1, 2015: LENS. CRACKED. EMERGENCY LIGHT AT MAIN CABIN DOOR FLOOR LEVEL, HAS A CRACKED LENS. DEFERRED IAW NEF 25-100-12.
- [SDR N6WA2015052700003](https://openairdocs.org/sdr/N6WA2015052700003), May 27, 2015: STOP FITTING. OUT OF ADJUST. MAIN CABIN DOOR INDICATION SHOWS OPEN. ADJUSTED PAX DOOR HANDLE STOP IAW AMM 52-11-02.
- [SDR N6WA2015042301](https://openairdocs.org/sdr/N6WA2015042301), Apr 23, 2015: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT ON LT SIDE HAS BULBS OUT. R & R LT EMER EXIT BULBS. OPERATIONS CHECKED GOOD IAW AMM 33-51-05.
- [SDR V0XD20150416101](https://openairdocs.org/sdr/V0XD20150416101), Apr 17, 2015: STRINGER. CORRODED. FORWARD AVIONICS COMPARTMENT, STRINGER 27R HAS CORROSION BETWEEN FS 333.00 TO 349.00. R & R STRINGER 25R, PN SH670-31212-2 IAW SRM 51-42-06, 51-40-11 & 51-25-16
- [SDR V0XD20150423113](https://openairdocs.org/sdr/V0XD20150423113), Apr 16, 2015: STRINGER. CORRODED. STRINGER 26R BETWEEN FS 333.0 & 349.0, IS CORRODED. R & R STRINGER 26R BETWEEN FS 333.0 & 349.0, PN SH670-31372-4 IAW SRM 51-42-06, 53-21-03, 51-21-11 & 51-40-1
- [SDR V0XD20150416105](https://openairdocs.org/sdr/V0XD20150416105), Apr 16, 2015: FRAME. CORRODED. CORROSION ON FRAME 333 AT STRINGER 27. CUT OUT CORRODED FRAME 333 FROM STRINGER 25L TO 25R, FABRICATED & INSTALLED REPAIR PARTS IAW REO 670-53-21-799, DATED 30 
- [SDR V0XD20150416104](https://openairdocs.org/sdr/V0XD20150416104), Apr 16, 2015: INTERCOSTAL. CORRODED. LEFT & RIGHT INTERCOSTAL AT FS 364.00 ARE CORRODED. LT & RT INTERCOSTAL AT FS 364.00, PNS SH670-32075-3 &-4, IAW SRM 51-42-06 & 51-42-21.
- [SDR V0XD20150416103](https://openairdocs.org/sdr/V0XD20150416103), Apr 16, 2015: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT AT FS 280.00 IN FWD AVIONICS COMPARTMENT IS CORRODED. R & R FLOOR SUPPORT, PN CC670-34256-3, IAW SRM 51-42-21, 51-40-11 & 51-42-06.
- [SDR V0XD20150416102](https://openairdocs.org/sdr/V0XD20150416102), Apr 16, 2015: MOUNT BRACKET. CORRODED. T CASS ANTENNA MOUNTING BRACKET CORRODED. R & R T CASS ANTENNA BRACKET, PN SH670-32364-7, IAW SRM 51-42-06, 51-40-11, 51-25-16, AMM 34-43-00 & 34-43-07.
- [SDR V0XD20150416098](https://openairdocs.org/sdr/V0XD20150416098), Apr 15, 2015: FRAME. CORRODED. FRAME 345.00 AT STRINGER 27 IS CORRODED. REPAIRED FRAME 345.00 AT STRINGER 27 BY CUTTING OUT CORRODED AREA & INSTALLING REPAIR PARTS IAW REO 670-53-21-1176 DATE
- [SDR V0XD20150406088](https://openairdocs.org/sdr/V0XD20150406088), Apr 13, 2015: SEAT TRACK. CORRODED. RIGHT FLOOR SEAT RAIL FROM FS 364.00 - 477.00 SHOWING SIGNS OF CORROSION. R & R SEAT RAIL, PN SH670-32159-1 IAW AMM 53-00-49 & SRM 53-21-49.
- [SDR V0XD20150406094](https://openairdocs.org/sdr/V0XD20150406094), Apr 12, 2015: ANGLE. CORRODED. SERVICE DOOR KICK ANGLE IS CORRODED. R & R SERVICE DOOR KICK ANGLE, PN SH670-31996-1, IAW SRM 51-42-06 & 51-42-21.
- [SDR V0XD20150511134](https://openairdocs.org/sdr/V0XD20150511134), Apr 11, 2015: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT AT FS 279.00 IS CORRODED. R & R FLOOR SUPPORT, PN CC670-33292-13, IAW SRM 51-42-06 & 51-40-11. WO 80282 & WC 2107.
- [SDR V0XD20150406092](https://openairdocs.org/sdr/V0XD20150406092), Apr 11, 2015: BULKHEAD. CORRODED. LEFT FS 280.00 BULKHEAD WEB CORRODED. REMOVED LT FS 280.00 BULKHEAD WEB, FABRICATED & INSTALLED NEW FS 280.00 BULKHEAD WEB IAW 670-53-11-594 DATED 27 APRIL 2011
- [SDR V0XD20150406091](https://openairdocs.org/sdr/V0XD20150406091), Apr 11, 2015: STRIKER. CORRODED. SERVICE DOOR SEAL STRIKER CORRODED. CORRECTIVE ACTION: REOMOVED AND REPLACED SERVICE DOOR SEAL STRIKER, PN:SH670-31412-3, IAW CRJ700 SRM 51-40-11, 51-41-00, 51-
- [SDR V0XD20150406090](https://openairdocs.org/sdr/V0XD20150406090), Apr 11, 2015: DOOR SILL. CORRODED. RIGHT FLOOR SILL FROM FS 280.00 TO THE SERVICE DOOR SHOWING SIGNS OF CORROSION. R & R RT SILL, PN SH670-32172-3 IAW SRM 51-21-11, 51-25-16, 51-42-20, 51-42-13, 
- [SDR V0XD20150406089](https://openairdocs.org/sdr/V0XD20150406089), Apr 11, 2015: BEAM. CRACKED. LEFT & RIGHT SIDE OF FS 280.00 BEAM CRACKED & CORRODED. R & R FS 280.00 BEAM PN CC670-34175-7S IAW SRM 53-11-41, 51-42-21, 51-42-06, 51-42-13 & AMM 20-70-00.
- [SDR V0XD20150406093](https://openairdocs.org/sdr/V0XD20150406093), Apr 9, 2015: ATTACH ANGLE. CORRODED. AFT WING TO BODY FAIRING WEB, ATTACH ANGLE IS CORRODED. R & R ANGLE, PNSH670-39189-1, IAW SRM 51-40-11, 51-42-06 & 51-42-15.
- [SDR V0XD20150410088](https://openairdocs.org/sdr/V0XD20150410088), Apr 9, 2015: ANGLE. CORRODED. PASSENGER DOOR CUT OUT SURROUND MID CAP ANGLE IS CORRODED. R & R MID CAP ANGLE IAW SRM 51-41-02.
- [SDR V0XD20150406087](https://openairdocs.org/sdr/V0XD20150406087), Apr 8, 2015: STRAP. CRACKED. AFT WING TO FUSELAGE FAIRING CTR STRAP IS CRACKED & CORRODED. R & R CTR STRAP, PN CC670-39251, IAW SRM 51-42-06 & 51-40-11.
- [SDR V0XD2015041600099](https://openairdocs.org/sdr/V0XD2015041600099), Apr 7, 2015: FLOORBEAM. CORRODED. AFT CARGO FLOORBEAM CORRODED AT FS 1030, LBL 27. R & R AFT FLOORBEAM SECTION IAW REO 670-53-00-029 REV A. NDT PERFORMED, NO CRACKS LOCATED.
- [SDR V0XD20150415097](https://openairdocs.org/sdr/V0XD20150415097), Apr 7, 2015: SEAT TRACK. CORRODED. LEFT SEAT TRACK 3, INBD HAS CORROSION BETWEEN FS 517.00 & FS 587.00, LT SEAT TRACK 4, INBD HAS CORROSION BETWEEN FS 581.00 & FS 629.00. BLENDED DAMAGE ON LT 4 S

All 121: https://openairdocs.org/aircraft/N642CA/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (53, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Cirrus Design SR22T)

- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA01134DE](https://openairdocs.org/stc/SA01134DE): Installation of EarthX ETX680-24-TSO Lithium Battery. EarthX Inc
- [STC SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Airwolf Filter Corporation
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA12274IB](https://openairdocs.org/stc/SA12274IB): Installation of the MT-Propeller Entwicklung GmbH MTV-9-D/198-52() and MTV-9-D/198-58() propellers. MT-Propeller Entwicklung GmbH
- [STC SA12064WI](https://openairdocs.org/stc/SA12064WI): Hardware and software updates for the Garmin G1000 Integrated Avionics System. Garmin International Inc
- [STC SA12080BO](https://openairdocs.org/stc/SA12080BO): Installation of Prodigy model 90901() LED Landing Light. Whelen Aerospace Technologies
- [STC SA12027IB](https://openairdocs.org/stc/SA12027IB): Installation of the MT-Propeller Entwicklung GmbH MTV-14-D/195-30() propeller. MT-Propeller Entwicklung GmbH
- [STC SA02924CH](https://openairdocs.org/stc/SA02924CH): Installation of M-T Propeller model MTV-14-D/195-30( ) 4 bladed propeller. McFarlane Aviation LLC
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02551AK](https://openairdocs.org/stc/SA02551AK): Installation of SKYDISPLAY Aircraft Interface Device (AID). AeroDisplay LLC
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA01076DE](https://openairdocs.org/stc/SA01076DE): Installation of main battery replacement with Concorde Valve Regulated Lead Acid battery. Concorde Battery Corporation
- [STC SA04440CH](https://openairdocs.org/stc/SA04440CH): Installation of Hartzell propeller model 4C1-F650A1/76C04-0.6 or 4C1-F650A1/76C04B-0.6. Hartzell Propeller Inc
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA04112CH](https://openairdocs.org/stc/SA04112CH): Installation of Appareo Systems, LLC Stratus ESG ADS-B transponder. Appareo Systems LLC
- [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation
- [STC SA00378BO](https://openairdocs.org/stc/SA00378BO): Installation of integrated wingtip exterior light assemblies. Cirrus Design Corporation
- [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley
- [STC SA03869NY](https://openairdocs.org/stc/SA03869NY): Installation of a Safetyplane Flight Monitoring System. ISEI International Services
- [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation
- [STC SA03777NY](https://openairdocs.org/stc/SA03777NY): Installation of RF-006(A) Main Wheel and RA-002(A) Nose Wheel with EA-003.3N Brake System. Beringer Aero
- [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC
- [STC SA11172SC](https://openairdocs.org/stc/SA11172SC): Installation of an ADS600-B Automatic Dependent Surveillance-Broadcast (ADS-B) Universal Access Transceiver (UAT) and Global Positioning System (GPS) antenna. NavWorx Inc
- [STC SA02554LA](https://openairdocs.org/stc/SA02554LA): Installation of a strut mounted Sensor Pod and wiring for a passenger operated monitoring system. Sky IMD Inc
- [STC SA02247SE](https://openairdocs.org/stc/SA02247SE): Removal of rear seats and installation of cargo shelf and restraint system. Tamarack Aerospace Group
- [STC SA04037CH](https://openairdocs.org/stc/SA04037CH): Installation of an Air Conditioning System, Kelly Aerospace kit #KATS-14-003. Installation Instructions as listed on NC-14 -022, revision D, dated November 19, 2015, and drawing list NC-14-021, revision D, dated September 24, 2015, or later FAA approved revision. Kelly Aerospace Thermal Systems LLC
- [STC SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc
- [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics
- [STC SA04154AT](https://openairdocs.org/stc/SA04154AT): Installation of a PM Firesystems LLC, Fire Suppression System. PM Fire Systems LLC
- [STC SA02442AK PAGE 1](https://openairdocs.org/stc/SA02442AK%20PAGE%201): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC
- [STC SA02283SE PAGE 1](https://openairdocs.org/stc/SA02283SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc
- [STC SA02402SE PAGE 1](https://openairdocs.org/stc/SA02402SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc
- [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc
- [STC SA00269BO](https://openairdocs.org/stc/SA00269BO): Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000. Avidyne Corporation
- [STC SA02717NY PAGE 1](https://openairdocs.org/stc/SA02717NY%20PAGE%201): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC
- [STC SA03372NY](https://openairdocs.org/stc/SA03372NY): Installation of RF-006(A) main wheel well and RA-002(A) nose wheel well with EA-003.4N(B) brake system. Beringer Aero
- [STC SA02825NY PAGE 1](https://openairdocs.org/stc/SA02825NY%20PAGE%201): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc
- [STC SA5156NM](https://openairdocs.org/stc/SA5156NM): Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System. AvTek
- [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc
- [STC SA2693NM](https://openairdocs.org/stc/SA2693NM): Installation of Electronics International digital volt/amp gauges and accessories. Electronics International Inc
- [STC SA02717NY](https://openairdocs.org/stc/SA02717NY) (historical): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC

### Approved for the engine (Continental TSIO-550-K)

- [STC SE03309CH](https://openairdocs.org/stc/SE03309CH): Installation of Engine Preheat Kit, p/n TSP6CYL-2927-115 for 115 volt application. Hartzell Propeller Inc
- [STC SE04577CH](https://openairdocs.org/stc/SE04577CH): Install an electronic engine ignition system. Electroair Acquisition Corp

All 53: https://openairdocs.org/aircraft/N642CA/stcs.md

## Earlier aircraft with N642CA

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N642CA before.

- [Cancelled 1991-06-25](https://openairdocs.org/deregistered/N642CA-1991-06-25): Piper PA-23-250, S/N 273144. Triennial form not returned. Owner: [Sawyer Alicia C](https://openairdocs.org/faa-owner/SAWYER%20ALICIA%20C), Marsh Harbr Abaco

## Related

- Other Cirrus Design SR22T aircraft: https://openairdocs.org/model/cirrus-design-sr22t/aircraft.md
- The Continental TSIO-550-K engine: https://openairdocs.org/engine/continental-tsio-550-k.md

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